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Analytical Investigation of the Reentry Behavior of the ''flying Wind Tunnel'' Test Vehicle, with Some Effects of Threshold and Torque Level of a Roll-rate Control SystemAnalytical investigation of reentry behavior of flying wind tunnel test vehicle with some effects of threshold and torque level of roll-rate control system
Document ID
19660030321
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Fletcher, H. S. (NASA Langley Research Center Hampton, VA, United States)
Jaquet, B. M. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1962
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-697
Report Number: NASA-TM-X-697
Accession Number
66N39611
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
CONTROL SYSTEM
REENTRY CONDITION

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